Tacoma Narrows Bridge (Galloping Gertie)
7 November 1940 · Puget Sound, WA
Long-span plate-girder-stiffened suspension (2,800 ft main span)

7 Nov 1940 — the 39-ft-wide, 8-ft-deep plate-girder deck in fully developed torsional flutter. The two curbs are at radically different elevations: the section is rotating about its centerline, not bending.
Photo: Washington State Archives / Wikimedia Commons (public domain)
Timeline
1 Jul 1940
Bridge opens; noticeable vertical oscillations from day one.
7 Nov 1940 · 10:00
Wind ~42 mph; motion transitions from vertical to torsional flutter.
11:00
Torsional amplitude exceeds 45°; deck twists in opposing directions between towers.
11:10
Suspender cables at midspan fail; central span collapses. No human fatalities (one dog).
Engineering root cause
Aeroelastic torsional flutter of an unusually slender H-section deck. Bluff cross-section shed vortices that resonated with the fundamental torsional mode.
Forensic findings
- Deck slenderness: L/d = 2,800/8 = 350, versus ≈ 85 for the Golden Gate. The section had almost no torsional stiffness (open H-section, GJ ≈ 0).
- The solid stiffening girders acted as a bluff body. Vortices shed at a frequency that locked in with the first antisymmetric torsional mode (0.2 Hz) — classic single-degree-of-freedom flutter, not simple resonance.
- Critical flutter wind speed was later back-computed at ≈ 35–42 mph. The design wind pressure had been treated as a static 30 psf — a strength check with no aerodynamic content whatsoever.
- Failure initiated when a north-side cable band slipped at midspan, converting the symmetric suspension geometry into an asymmetric one and removing the last torsional restraint.
What it changed in the code
Every long-span suspension/cable-stayed deck now undergoes wind-tunnel section-model testing; AASHTO requires aeroelastic evaluation and requires dynamic analysis for flexible structures.
What you do differently today
- Section-model wind-tunnel testing is mandatory for any deck with a span-to-depth ratio above ~150 or a fundamental frequency below 1 Hz.
- Use a torsionally closed section (box girder) or add an open truss deck with grating to bleed pressure — both raise the critical flutter speed.
- Check flutter, vortex-induced vibration, galloping and buffeting separately; passing one does not imply the others.
- AASHTO §3.8.3 requires that aeroelastic instability not occur below the design wind speed with a margin; §C4.6.5 governs the dynamic model.







